smoke detection Flashcards

1
Q

Benefit of detecting smoke

A

it’s an early indication of fire

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2
Q

Where are smoke detectors placed

A

Cargo holds

toilets

Avionics bay

crew rest area

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3
Q

TRaingle - fire causing agents

A
  • source of ignition
  • fuel
  • oxygen

Take any of the three away, and fire will go out

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4
Q

Categorization

A

Level of smoke and fire detection depends on ‘accessibility of the compartments
- How easy the are to access and fix the problem

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5
Q

2 Types of ‘smoke’ detection systems

A

Optical

Ionizing

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6
Q

Optical detection

A

Detector is comprised of a light source and sensor arranged in this manner:

In normal conditions
* The sensor can’t detect light source

In smoke condition (particles are present)
* light reflects off the particles and is detected by the sensor
* ** Two or more detectors both sensing** the smoke simultaneously will trigger an alarm
* a labyrinth optical detector - light reflects towards the photsensitive cell and the labyrinth has a shield

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7
Q

How to test if smoke detector is working

A

In cargo smoke panel, you can test by doing this:

  1. once you press the test button
  2. test lamp shines at the sensor
  3. this triggers the signal and illuminates the caption
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8
Q

Ionizing

A

A system with ionizing chambers

contains radio active material that emit **alpha particles - they ionize the air **in the chambers.

In normal conditions:
* a potential difference in ionized air allows a small electrical current to flow between the plates of the dector

In smoke conditions
* smoke particles enter the chamber.
* They get absorbed by alpha particles
* ionization level decreases, consequently the current flow decreaes
* Once current flow drops to a certain leve, a warning is triggered.

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9
Q

Fire detection and extinguishing system in
2 key areas

A

cargo compartment

engine bay

main wheel wells

Auxillary power unit

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10
Q

3 vulnerable zones in an engine bay

A

IN A 3 ZONE SYSTEM
Requires both fire detection and extinguisher

Zone 1 - Most sensitive to fire
Area of hydraulic pumps, fuel pumps, fuel control unit

Zone 2
compressor & fan area
uncontained blade area can cause fire
Generates more heat than zone 1

Zone 3
combustion and turbine sections

Each zone is spearated by fire proof Bulkhead/FIREWALLS - stainless steel or titanium

IN A 2 ZONE SYSTEM
Zone 1 & 2 = Cool zone
Zone 3 = Hot zone

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11
Q

Auxillary Power Unit
Also an engine

A
  • APU bay - located at the back of the aircraft
  • Has it’s own fire detection and protection system
  • Automatic
  • APU shuts down in case of fire
  • Zone 1
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12
Q

Engine Fire detection systems

A

Continuous Loop

Gas filled detector

Bimetallic Overheat sensors

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13
Q

Continous Loop Engine Fire Detection System (FIRE WIRE)

A

Operates on the principle of:
* Wire to detect resistance and capacitance when heated
* Therefore there is a

Composed of:
1. Controller monitor
2. Detection loops (stainless steel, salt,nickle core)
* negative coefficient of resistance loop
* positiove coefficient of capacitance loop

Location:
* engine nacelles
* loops are wound around engine components on the engine casing

**Each engine is equipped with: **
* A pair of fire detection loops
* A pair of overheat detection loops

Set up:
2 loops are used: Loop A & Loop B
independent of each other
have their own detection controller

How it works - in resistance system
* current flows in a continuous loop
* If temp rises, the salt resistance reduces
* flow of current between electrode and out tube increases
* At a predetermined temperature, sufficient current will flow and warning system will operate
* If temp drops to a certail value, the system will reset and alarm stops
* This works when there is an isolated temperature increase due to hot gas leak or fire

How it works - in capacitance system
* current flows in a continuous loop
* If temp rises, the capacitance increase
* feedback current increases
* when it increases at a predetermined level, warning system will operate
* If temp drops to a preset value, the system will reset and alarm stops
* This works when there is an isolated temperature increase due to hot gas leak or fire

Detecting faults:
* short circuit between the case and inner elctrode may give a false fire warning
* When a disrepency cannot detect heat
* Ex: If there is a rapid decrease in resistance and corresponding increase in capacitance

Fault Alert
* Amber FAULT caption is illuminated for the relevant loop A or Loop B push button
* Amber Loop light illuminates

What to do after seeing the alert
* Selecting the faulty loop off restores the fire detection capability.
* You must isolate the defective loop because a malfunctioning loop that isn’t turned off, will prevent proper fire alerting

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14
Q

Continous Loop Engine Fire Detection FAULT

A

Scenario 1:
(low resitance) and (low capacity)
(fire) and (no fire) = fault

Scenarion 2:
Sensing element is crushed, inner core doesn’t touch the other casing

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15
Q

Continous Loop Engine Fire Detection FAULT/Alarm/no effect

A

Scenario 1: FAULT
(low resitance) and (low capacity)
(fire) and (no fire)

Scenario 2: No Reaction
Sensing element is crushed, inner core doesn’t touch the other casing

Scenarion 3: fire alarm is triggered
Inner core contacts the outer casing

Scenario 4: fire alarm is triggered
Sensing element is crushed,casing is touched

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16
Q

Bimetallic overheat sensors

A

Located in:
* Used to protect curcial spots on the airframe

Operates on the principle of:
* different metals have different coefficient of expansion

Composed of:
* Outer sensor containing 2 metallic strips with low coefficient of expansion
* metallic strips have an electrical contact each

How it works
* In normal conditions: strips are lightly compressed
* When heated: outer sensor expands, inner strips stretch, contact points touch
* A circuit is created –>signal to flight deck

Notes
May cause slight delay before signal is given
this is to prevent false warning due to vibration

17
Q

Gas filled detectors

A

Comprised of:
* Responder Unit with
* 2 pressure switches
* 2 loops (titanium hydride and helium)

How it works

In normal conditions
* gas pressure is 7psi
* gas is connected to the switches in the respondor unit
* Gas operates on averaging gas pressure switch that holds the system integreity switch closed and** alarm switch is open**

If loop breaks - system fault
* helium gas will be released from the core
* Drop in pressure
* opens the integrity switch ->signals fault

If there is spread heat over an area
* the temperature increase is less than the one created by a flame
* But it will be felt by a larger area
* so hydrogen is not going to be released.
* but pressure increase in helium gas
* Closes the alarm switch ->signals fire

if there is fire (localized)
* heat releases hydroge gas from the titanium hydride
* temperature felt locallly (ie local area)
* pressure increases to 40psi
* Closes the alarm switch ->signals fire

18
Q

Fire warning controls

A
  1. illuminated FIRE master warning caption in Flashing Red
  2. warning bell
  3. Eng 1 or Eng 2 steady illuminated caption
  4. appropriate extinguisher operating handle illuminated
  5. Display **warning on EICAS or ECAM **

TEST BUTTON
- when pressed should indicate with a red light (means it’s working)
- if no alarm (test failed)

In continous loop detector
if a break between core and outer tube, then no alarm is given (test failed)
can still fly if 1 loop fails in flight. System switches to 1 loop operation (limited # of sector of flights)

In an gas filled detector
if integrity switch detector is open, no alarm is given (test failed)

19
Q

Engine fire extinguisher (Power Plant)

A

2 bottle (2-shot) system on the wing (or cargo compartment)

Each bottle can send extinguisher to either engines

required by law

either engine is capable of receiving a total of 2 shots of extinguisher

filled with HALON (BCF or BTM)

TOILET:
* Also ther is a built in fire extinguisher in the toilet towel disposer.

  • It is triggered by heat not smoke
20
Q

what happens when you pull the fire handle for the affected engine?

A

by PILOT ACTION

Closes:
* the shut off valve in wing spar to isolate the fuel system
* the air bleed PRSOV
* hyrdraulic pump
* APU shut off valve
* closing of hte isolation and de-icing valves

Isolate
* hydraulic fluid
* engine drive electric generator

Arms
* extinguisher squibs ready for release

21
Q

how it works

A

When the fire handle is rotated, the extinguisher bottle fires (electrically) and ruptures a retaining disc in the valve
This forces the piston to move in the squib to release the liquid agent and turns into gas

Each squib feeds a particular engine.

on each bottle (L and R)
Squib L for Engine 1
Squib R for Engine 2

Engine 1:
rotate anti clock wise
activate squib L
discharge contant into Eng 1.
Bottle L can no longer be used after discharge

Rotate fire handle clock wise
activate squib R
discharge contant into Eng 1.
Bottle R can no longer be used after discharge

If a bottle has been discharged into one engine, the bottole can no longer be used for the other engine

22
Q

what are ‘photoelectric cells’

A

smoke detectors

detect the diffusion of a beam of light which occurs when the beam is interrupted by smoke.

the scattering of the light increases the ‘conductance’ of the cell and its outp is amplified to operate a warning circuit